NAS 1.15:86788
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Practical aspects of laser holographic interferometry wind tunnels |
1 |
NAS 1.15:86789
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NASA rotor systems research aircraft fixed-wing configuration flight-test results |
1 |
NAS 1.15:86790
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High-angle-of-attack pneumatic lag and upwash corrections for a hemispherical flow direction sensor |
1 |
NAS 1.15:86791
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Description of an experimental expert system flight status monitor |
1 |
NAS 1.15:86793
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Highly integrated digital electronic control, digital flight control, aircraft model identification and adaptive engine control |
1 |
NAS 1.15:86795
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NAS 1.15:86798
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Buckling behavior of René 41 tubular panels for a hypersonic aircraft wing |
1 |
NAS 1.15:86799
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NAS 1.15:86800
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Effects of forced and free convections on structural temperatures of shuttle orbiter during reentry flight |
1 |
NAS 1.15:86801
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Decoupling control synthesis for an oblique-wing aircraft |
1 |
NAS 1.15:86802
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Development of a knowledege acquisition tool for an expert system flight status monitor |
1 |
NAS 1.15:86803
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Dynamics and controls flight testing of the X-29A airplane |
1 |
NAS 1.15:86804
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Bibliography for aircraft parameter estimation |
1 |
NAS 1.15:86805
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The role of a real-time flight support facility in flight research programs |
1 |
NAS 1.15:86806
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Comparison of theoretical and flight-measured local flow aerodynamics for a low-aspect-ratio fin |
1 |
NAS 1.15:86807
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Flight test of a resident backup software system |
1 |
NAS 1.15:86808
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Aeroelastic control of oblique-wing aircraft |
1 |
NAS 1.15:86809
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X-29A technology demonstrator flight trest program overview |
1 |
NAS 1.15:86811
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Summary of results of NASA F-15 flight research program |
1 |
NAS 1.15:86812
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Prediction of service life of aircraft structural components using the half-cycle method |
1 |